Influence of angles and hole pitches on discharge coefficients of expanded holes at inlet and outlet

Guang Chao Li, Hui Ren Zhu, Hui Ming Fan

Research output: Contribution to journalArticlepeer-review

5 Scopus citations

Abstract

This paper presented discharge coefficients of the expanded holes at inlet and outlet with plane angles of 20°, 45°, 90°, radial angles of 0°, 30°, 65° and the ratios of pitch to diameter of 2, 3, 4. The momentum flux ratios varied in the range from 1 to 8. The results show that discharge coefficients of radial angle =0° increase significantly when the plane angles increase from 20° to 90°. The effect of plane angle becomes weak with the increasing radial angles. Radial angles have weak influence on the discharge coefficients of plane angle=20° and discharges coefficients of plane angle=45° and plane angle=90° decreases when the radial angles increase from 0° to 65°. Discharge coefficients of plane angle=90° increase when the ratios of hole pitch to the diameter increase from 2 to 4.

Original languageEnglish
Pages (from-to)499-506
Number of pages8
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume24
Issue number3
StatePublished - Mar 2009

Keywords

  • Discharge coefficient
  • Experiment
  • Film cooling
  • Turbine

Fingerprint

Dive into the research topics of 'Influence of angles and hole pitches on discharge coefficients of expanded holes at inlet and outlet'. Together they form a unique fingerprint.

Cite this